View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 85U 61004C 25082.75089604 .00213831 00000-0 92297-2 0 9999
2 85 38.6819 241.1569 0084810 203.0349 156.6613 15.17633425181768
| Epoch (UTC): | 23 March 2025 18:01:17 |
| Eccentricity: | 0.0084810 |
| inclination: | 38.6819° |
| perigee height: | 454 km |
| apogee height: | 571 km |
| right ascension of ascending node: | 241.1569° |
| argument of perigee: | 203.0349° |
| revolutions per day: | 15.17633425 |
| mean anomaly at epoch: | 156.6613° |
| orbit number at epoch: | 18176 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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